EP2192271A3 - Mittelturbinenrahmen einer Gasturbine - Google Patents
Mittelturbinenrahmen einer Gasturbine Download PDFInfo
- Publication number
- EP2192271A3 EP2192271A3 EP09252349A EP09252349A EP2192271A3 EP 2192271 A3 EP2192271 A3 EP 2192271A3 EP 09252349 A EP09252349 A EP 09252349A EP 09252349 A EP09252349 A EP 09252349A EP 2192271 A3 EP2192271 A3 EP 2192271A3
- Authority
- EP
- European Patent Office
- Prior art keywords
- outer case
- spokes
- load transfer
- mid
- gas turbine
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Granted
Links
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
- F01D25/00—Component parts, details, or accessories, not provided for in, or of interest apart from, other groups
- F01D25/16—Arrangement of bearings; Supporting or mounting bearings in casings
- F01D25/162—Bearing supports
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
- F01D25/00—Component parts, details, or accessories, not provided for in, or of interest apart from, other groups
- F01D25/24—Casings; Casing parts, e.g. diaphragms, casing fastenings
- F01D25/243—Flange connections; Bolting arrangements
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
- F01D25/00—Component parts, details, or accessories, not provided for in, or of interest apart from, other groups
- F01D25/28—Supporting or mounting arrangements, e.g. for turbine casing
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
- F01D9/00—Stators
- F01D9/06—Fluid supply conduits to nozzles or the like
- F01D9/065—Fluid supply or removal conduits traversing the working fluid flow, e.g. for lubrication-, cooling-, or sealing fluids
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
- F05B—INDEXING SCHEME RELATING TO WIND, SPRING, WEIGHT, INERTIA OR LIKE MOTORS, TO MACHINES OR ENGINES FOR LIQUIDS COVERED BY SUBCLASSES F03B, F03D AND F03G
- F05B2260/00—Function
- F05B2260/30—Retaining components in desired mutual position
- F05B2260/301—Retaining bolts or nuts
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
- F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
- F05D2230/00—Manufacture
- F05D2230/60—Assembly methods
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
- F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
- F05D2240/00—Components
- F05D2240/10—Stators
- F05D2240/11—Shroud seal segments
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
- F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
- F05D2240/00—Components
- F05D2240/55—Seals
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
- F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
- F05D2260/00—Function
- F05D2260/94—Functionality given by mechanical stress related aspects such as low cycle fatigue [LCF] of high cycle fatigue [HCF]
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Physics & Mathematics (AREA)
- Fluid Mechanics (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US12/324,977 US8091371B2 (en) | 2008-11-28 | 2008-11-28 | Mid turbine frame for gas turbine engine |
Publications (3)
| Publication Number | Publication Date |
|---|---|
| EP2192271A2 EP2192271A2 (de) | 2010-06-02 |
| EP2192271A3 true EP2192271A3 (de) | 2012-12-26 |
| EP2192271B1 EP2192271B1 (de) | 2014-09-03 |
Family
ID=41259448
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| EP09252349.7A Active EP2192271B1 (de) | 2008-11-28 | 2009-10-01 | Gasturbinenmotor |
Country Status (3)
| Country | Link |
|---|---|
| US (1) | US8091371B2 (de) |
| EP (1) | EP2192271B1 (de) |
| CA (1) | CA2672329C (de) |
Families Citing this family (113)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US8128021B2 (en) | 2008-06-02 | 2012-03-06 | United Technologies Corporation | Engine mount system for a turbofan gas turbine engine |
| US20140174056A1 (en) | 2008-06-02 | 2014-06-26 | United Technologies Corporation | Gas turbine engine with low stage count low pressure turbine |
| US8251651B2 (en) * | 2009-01-28 | 2012-08-28 | United Technologies Corporation | Segmented ceramic matrix composite turbine airfoil component |
| US9631558B2 (en) | 2012-01-03 | 2017-04-25 | United Technologies Corporation | Geared architecture for high speed and small volume fan drive turbine |
| US9239012B2 (en) | 2011-06-08 | 2016-01-19 | United Technologies Corporation | Flexible support structure for a geared architecture gas turbine engine |
| US9410608B2 (en) | 2011-06-08 | 2016-08-09 | United Technologies Corporation | Flexible support structure for a geared architecture gas turbine engine |
| US9458721B2 (en) * | 2011-09-28 | 2016-10-04 | United Technologies Corporation | Gas turbine engine tie rod retainer |
| US8979484B2 (en) | 2012-01-05 | 2015-03-17 | Pratt & Whitney Canada Corp. | Casing for an aircraft turbofan bypass engine |
| US9316117B2 (en) * | 2012-01-30 | 2016-04-19 | United Technologies Corporation | Internally cooled spoke |
| US9816442B2 (en) | 2012-01-31 | 2017-11-14 | United Technologies Corporation | Gas turbine engine with high speed low pressure turbine section |
| US8887487B2 (en) | 2012-01-31 | 2014-11-18 | United Technologies Corporation | Geared turbofan gas turbine engine architecture |
| US9255487B2 (en) | 2012-01-31 | 2016-02-09 | United Technologies Corporation | Gas turbine engine seal carrier |
| US20150345426A1 (en) | 2012-01-31 | 2015-12-03 | United Technologies Corporation | Geared turbofan gas turbine engine architecture |
| US9140137B2 (en) | 2012-01-31 | 2015-09-22 | United Technologies Corporation | Gas turbine engine mid turbine frame bearing support |
| US10287914B2 (en) | 2012-01-31 | 2019-05-14 | United Technologies Corporation | Gas turbine engine with high speed low pressure turbine section and bearing support features |
| US10240526B2 (en) | 2012-01-31 | 2019-03-26 | United Technologies Corporation | Gas turbine engine with high speed low pressure turbine section |
| US8935913B2 (en) | 2012-01-31 | 2015-01-20 | United Technologies Corporation | Geared turbofan gas turbine engine architecture |
| US9835052B2 (en) * | 2012-01-31 | 2017-12-05 | United Technologies Corporation | Gas turbine engine with high speed low pressure turbine section and bearing support features |
| US20130192196A1 (en) * | 2012-01-31 | 2013-08-01 | Gabriel L. Suciu | Gas turbine engine with high speed low pressure turbine section |
| US9611859B2 (en) * | 2012-01-31 | 2017-04-04 | United Technologies Corporation | Gas turbine engine with high speed low pressure turbine section and bearing support features |
| US9222417B2 (en) | 2012-01-31 | 2015-12-29 | United Technologies Corporation | Geared turbofan gas turbine engine architecture |
| US9845726B2 (en) | 2012-01-31 | 2017-12-19 | United Technologies Corporation | Gas turbine engine with high speed low pressure turbine section |
| US20130192191A1 (en) | 2012-01-31 | 2013-08-01 | Frederick M. Schwarz | Gas turbine engine with high speed low pressure turbine section and bearing support features |
| US10125693B2 (en) | 2012-04-02 | 2018-11-13 | United Technologies Corporation | Geared turbofan engine with power density range |
| US10138809B2 (en) | 2012-04-02 | 2018-11-27 | United Technologies Corporation | Geared turbofan engine with a high ratio of thrust to turbine volume |
| US8756908B2 (en) | 2012-05-31 | 2014-06-24 | United Technologies Corporation | Fundamental gear system architecture |
| US20150308351A1 (en) | 2012-05-31 | 2015-10-29 | United Technologies Corporation | Fundamental gear system architecture |
| US8572943B1 (en) | 2012-05-31 | 2013-11-05 | United Technologies Corporation | Fundamental gear system architecture |
| US9851008B2 (en) * | 2012-06-04 | 2017-12-26 | United Technologies Corporation | Seal land for static structure of a gas turbine engine |
| US9394915B2 (en) * | 2012-06-04 | 2016-07-19 | United Technologies Corporation | Seal land for static structure of a gas turbine engine |
| EP2672071A1 (de) | 2012-06-08 | 2013-12-11 | Siemens Aktiengesellschaft | Ablaufleitungsanordnung und Gasturbinenmotor mit einer Ablaufleitungsanordnung |
| US8863531B2 (en) * | 2012-07-02 | 2014-10-21 | United Technologies Corporation | Cooling apparatus for a mid-turbine frame |
| US9222413B2 (en) | 2012-07-13 | 2015-12-29 | United Technologies Corporation | Mid-turbine frame with threaded spokes |
| US9217371B2 (en) | 2012-07-13 | 2015-12-22 | United Technologies Corporation | Mid-turbine frame with tensioned spokes |
| US9587514B2 (en) | 2012-07-13 | 2017-03-07 | United Technologies Corporation | Vane insertable tie rods with keyed connections |
| US9212556B2 (en) | 2012-08-21 | 2015-12-15 | United Technologies Corporation | Multifunction positioning lock washer |
| EP2900973B1 (de) * | 2012-09-28 | 2018-12-12 | United Technologies Corporation | Mittelturbinenrahmen mit verkleidungsbefestigung |
| US9903224B2 (en) | 2012-12-29 | 2018-02-27 | United Technologies Corporation | Scupper channelling in gas turbine modules |
| JP6271582B2 (ja) | 2012-12-29 | 2018-01-31 | ユナイテッド テクノロジーズ コーポレイションＵｎｉｔｅｄ Ｔｅｃｈｎｏｌｏｇｉｅｓ Ｃｏｒｐｏｒａｔｉｏｎ | ガスタービンシールアセンブリおよびシール支持体 |
| US10053998B2 (en) | 2012-12-29 | 2018-08-21 | United Technologies Corporation | Multi-purpose gas turbine seal support and assembly |
| WO2014105599A1 (en) | 2012-12-29 | 2014-07-03 | United Technologies Corporation | Heat shield for cooling a strut |
| WO2014105657A1 (en) | 2012-12-29 | 2014-07-03 | United Technologies Corporation | Mount with deflectable tabs |
| DE112013006258B4 (de) | 2012-12-29 | 2026-01-15 | RTX Corporation (n.d.Ges.d. Staates Delaware) | Turbinenrahmenanordnung und Verfahren zum Bereitstellen einer Turbinenrahmenanordnung |
| WO2014105800A1 (en) | 2012-12-29 | 2014-07-03 | United Technologies Corporation | Gas turbine seal assembly and seal support |
| WO2014105100A1 (en) | 2012-12-29 | 2014-07-03 | United Technologies Corporation | Bumper for seals in a turbine exhaust case |
| EP2938836B1 (de) | 2012-12-29 | 2020-02-05 | United Technologies Corporation | Dichtungsträgerscheibe und anordnung |
| EP2938847B1 (de) * | 2012-12-29 | 2019-08-07 | United Technologies Corporation | Installationshalterung für ein turbinenabgasgehäuse |
| WO2014105602A1 (en) | 2012-12-29 | 2014-07-03 | United Technologies Corporation | Heat shield for a casing |
| US9631517B2 (en) | 2012-12-29 | 2017-04-25 | United Technologies Corporation | Multi-piece fairing for monolithic turbine exhaust case |
| WO2014105616A1 (en) * | 2012-12-29 | 2014-07-03 | United Technologies Corporation | Turbine exhaust case architecture |
| WO2014105603A1 (en) | 2012-12-29 | 2014-07-03 | United Technologies Corporation | Multi-piece heat shield |
| EP2938863B1 (de) | 2012-12-29 | 2019-09-25 | United Technologies Corporation | Mechanische verbindung für segmentierten hitzeschild |
| WO2014105619A1 (en) * | 2012-12-29 | 2014-07-03 | United Technologies Corporation | Multi-function boss for a turbine exhaust case |
| WO2014137444A2 (en) | 2012-12-29 | 2014-09-12 | United Technologies Corporation | Multi-ply finger seal |
| EP2938868B1 (de) | 2012-12-29 | 2019-08-07 | United Technologies Corporation | Anordnung zur strömungsumlenkung |
| WO2014105604A1 (en) | 2012-12-29 | 2014-07-03 | United Technologies Corporation | Angled cut to direct radiative heat load |
| WO2014105525A1 (en) * | 2012-12-29 | 2014-07-03 | United Technologies Corporation | Multi-purpose mounting |
| US10240532B2 (en) | 2012-12-29 | 2019-03-26 | United Technologies Corporation | Frame junction cooling holes |
| JP6249499B2 (ja) * | 2012-12-31 | 2017-12-20 | ユナイテッド テクノロジーズ コーポレイションＵｎｉｔｅｄ Ｔｅｃｈｎｏｌｏｇｉｅｓ Ｃｏｒｐｏｒａｔｉｏｎ | タービン排気ケースのマルチピース型フレーム |
| WO2014105716A1 (en) | 2012-12-31 | 2014-07-03 | United Technologies Corporation | Turbine exhaust case multi-piece frame |
| EP2938860B1 (de) * | 2012-12-31 | 2018-08-29 | United Technologies Corporation | Turbinenabgasgehäuse mit mehrteiligem rahmen |
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2009
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- 2009-10-01 EP EP09252349.7A patent/EP2192271B1/de active Active
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Also Published As
| Publication number | Publication date |
|---|---|
| CA2672329A1 (en) | 2010-05-28 |
| US8091371B2 (en) | 2012-01-10 |
| CA2672329C (en) | 2012-10-02 |
| EP2192271B1 (de) | 2014-09-03 |
| US20100132376A1 (en) | 2010-06-03 |
| EP2192271A2 (de) | 2010-06-02 |
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